Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:jet_engine
|
| gptkbp:aircraft_operated |
gptkb:fighter_aircraft
|
| gptkbp:compression_ratio |
6:1
|
| gptkbp:country_of_origin |
gptkb:Soviet_Union
|
| gptkbp:diameter |
0.9 m
|
| gptkbp:engine |
Brayton cycle
|
| gptkbp:engine_configuration |
axial flow
|
| gptkbp:first_flight |
gptkb:1955
|
| gptkbp:fuel_type |
kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
Tumansky R-25
|
| gptkbp:length |
3.5 m
|
| gptkbp:manufacturer |
Tumansky
|
| gptkbp:operational_use |
1960s
|
| gptkbp:propulsion |
25 k N
|
| gptkbp:replaced_by |
gptkb:Tumansky_R-29
|
| gptkbp:successor |
gptkb:Tumansky_R-29
|
| gptkbp:type |
turbojet
|
| gptkbp:used_in |
gptkb:Mikoyan-Gurevich_Mi_G-21
|
| gptkbp:weight |
300 kg
|
| gptkbp:bfsParent |
gptkb:Tumansky_R-15
gptkb:Tumansky_R-11 |
| gptkbp:bfsLayer |
6
|